Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane
By: Dennis O. Allision and William G. Sewall.
Contributors: Sewall, William G.; Langley Research Center.
Series: NASA technical paper -- 3516.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service (NTIS) [distributor
Published: 1995
Place of publication: Hampton, Va; Springfield, VA
Language: eng
Format: Microform
Subjects: Aircraft models.; Airfoils.; Leading edges.; Maneuverability.; Pressure distribution.; Subsonic speed.; Trailing edges.; Transonic speed.; Wind tunnel tests.; Wing-fuselage stores.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 95-0744-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 1 microfiche.